Distributed adaptive event-triggered control for attitude synchronization of multiple spacecraft
This paper investigates the problem of attitude synchronization tracking of multiple
spacecraft in the presence of limited inter-spacecraft communication, model uncertainties …
spacecraft in the presence of limited inter-spacecraft communication, model uncertainties …
Decentralized finite-time attitude synchronization for multiple rigid spacecraft via a novel disturbance observer
Q Zong, S Shao - Isa Transactions, 2016 - Elsevier
This paper investigates decentralized finite-time attitude synchronization for a group of rigid
spacecraft by using quaternion with the consideration of environmental disturbances, inertia …
spacecraft by using quaternion with the consideration of environmental disturbances, inertia …
Decentralized adaptive control for attitude synchronization of multiple spacecraft via quantized information exchange
This paper investigates the problem of decentralized attitude synchronization and tracking
for a group of spacecraft, whose communication topology is undirected, subject to inter …
for a group of spacecraft, whose communication topology is undirected, subject to inter …
Rotation matrix based finite-time attitude synchronization control for spacecraft with external disturbances
B Huang, A Li, Y Guo, C Wang - ISA transactions, 2019 - Elsevier
This paper investigates the anti-unwinding finite-time attitude synchronization control
problem for Spacecraft formation flying with external disturbances. Two finite-time controllers …
problem for Spacecraft formation flying with external disturbances. Two finite-time controllers …
[HTML][HTML] Distributed fixed-time attitude coordinated control for multiple spacecraft with actuator saturation
GAO Han, XIA Yuanqing, X Zhang, G Zhang - Chinese Journal of …, 2022 - Elsevier
This paper investigates the distributed fixed-time attitude coordinated control problem for
multiple spacecraft subject to actuator saturation under the directed topology. First, a …
multiple spacecraft subject to actuator saturation under the directed topology. First, a …
A novel attitude-tracking control for spacecraft networks with input delays
This article is concerned with the attitude synchronous tracking control of time-delayed
multispacecraft systems. The attitude-tracking error dynamics are transformed into a …
multispacecraft systems. The attitude-tracking error dynamics are transformed into a …
Fixed‐time attitude tracking control for spacecraft based on adding power integrator technique
B Jiang, C Li, S Hou, G Ma - International Journal of Robust …, 2020 - Wiley Online Library
In this article, the fixed‐time attitude tracking problem for rigid spacecraft is investigated
based on the adding‐a‐power‐integrator control technique. First, a fixed‐time attitude …
based on the adding‐a‐power‐integrator control technique. First, a fixed‐time attitude …
Distributed attitude control for multiple flexible spacecraft under actuator failures and saturation
D Huang, Q Wang, Z Duan - Nonlinear Dynamics, 2017 - Springer
This paper solves the problem of attitude consensus for flexible spacecraft formation under
actuator failures and saturation constraints. Three insightful distributed consensus control …
actuator failures and saturation constraints. Three insightful distributed consensus control …
Finite time coordinated formation control for spacecraft formation flying under directed communication topology
D Ran, X Chen, AK Misra - Acta Astronautica, 2017 - Elsevier
This paper investigates the finite time coordinated formation control problem for spacecraft
formation flying (SFF) under the assumption of directed communication topology. By using …
formation flying (SFF) under the assumption of directed communication topology. By using …
Attitude synchronization for multiple 3-DOF helicopters with actuator faults
The attitude synchronization for multiple three-degree-of-freedom helicopters in the
presence of system uncertainties and time-varying actuator faults is investigated. A fault …
presence of system uncertainties and time-varying actuator faults is investigated. A fault …